Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft

Jirui Yu, Ping Ruan, Yang Su, Yi-Jing He, Jin-you Tao, Zhe Zhang, Song Guo, Bin Xue, Jian Feng Yang
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Abstract

For the ASO-S/HXI payload, the accuracy of the flare reconstruction is reliant on important factors such as the alignment of the dual grating and the precise measurement of observation orientation. To guarantee optimal functionality of the instrument throughout its life cycle, the SAS is imperative to ensure that measurements are accurate and reliable. This is achieved by capturing the target motion and utilizing a physical model-based inversion algorithm. However, the SAS optical system's inversion model is a typical ill-posed inverse problem due to its optical parameters, which results in small target sampling errors triggering unacceptable shifts in the solution. To enhance inversion accuracy and make it more robust against observation errors, we suggest dividing the inversion operation into two stages based on the SAS spot motion model. Firstly, the as-rigid-as-possible (ARAP) transformation algorithm calculates the relative rotations and an intermediate variable between the substrates. Secondly, we solve an inversion linear equation for the relative translation of the substrates, the offset of the optical axes, and the observation orientation. To address the ill-posed challenge, the Tikhonov method grounded on the discrepancy criterion and the maximum a posteriori (MAP) method founded on the Bayesian framework are utilized. The simulation results exhibit that the ARAP method achieves a solution with a rotational error of roughly ±3.5 arcsec (1/2-quantile); both regularization techniques are successful in enhancing the stability of the solution, the variance of error in the MAP method is even smaller - it achieves a translational error of approximately ±18μm (1/2-quantile) in comparison to the Tikhonov method's error of around ±24μm (1/2-quantile). Furthermore, the SAS practical application data indicates the method's usability in this study. Lastly, this paper discusses the intrinsic interconnections between the regularization methods.
ASO-S 航天器上 HXI 有效载荷的太阳视角系统 (SAS) 的逆计算和正则化过程
对于 ASO-S/HXI 有效载荷来说,耀斑重建的准确性取决于双光栅的对准和观测方位的精确测量等重要因素。为了保证仪器在整个生命周期内发挥最佳功能,SAS 必须确保测量的准确性和可靠性。这可以通过捕捉目标运动并利用基于物理模型的反演算法来实现。然而,由于光学参数的原因,SAS 光学系统的反演模型是一个典型的非定常反演问题,导致微小的目标采样误差就会引发解的不可接受的偏移。为了提高反演精度,使其对观测误差具有更强的鲁棒性,我们建议根据 SAS 光斑运动模型将反演操作分为两个阶段。首先,尽可能刚性(ARAP)转换算法计算基底之间的相对旋转和中间变量。其次,我们求解基板相对平移、光轴偏移和观测方向的反演线性方程。为了解决这一难题,我们采用了基于差异准则的 Tikhonov 方法和基于贝叶斯框架的最大后验(MAP)方法。模拟结果表明,ARAP 方法获得的解的旋转误差约为±3.5 弧秒(1/2-四分位);两种正则化技术都成功地增强了解的稳定性,而 MAP 方法的误差方差更小--它获得的平移误差约为±18μm(1/2-四分位),而 Tikhonov 方法的误差约为±24μm(1/2-四分位)。此外,SAS 的实际应用数据也表明了该方法在本研究中的可用性。最后,本文讨论了正则化方法之间的内在联系。
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